BOEING 777 Hard Landing vertical G criteria
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BOEING 777 Hard Landing vertical G criteria
What is the G factor requiring hard landing checks by maintenance with aircraft being below max landing weight?
I saw an AMM chart that indicates 1.5 ish for the beginning of checks envelope.
Pertinent to mention that the note in the chart said something like this;
Load factor = Vertg + 1g
Anyone has references to elaborate the scenario?
I saw an AMM chart that indicates 1.5 ish for the beginning of checks envelope.
Pertinent to mention that the note in the chart said something like this;
Load factor = Vertg + 1g
Anyone has references to elaborate the scenario?
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At Zero roll angle the G Factor is 1.2
Determination of a Hard Landing check is done by the Flight Crew. MM 05-51-01 P201
(2) The flight crew must make a determination if a hard landing has occurred.
I would give you a picture of the chart but as a newby I'm not allowed to post attachments - sorry
Determination of a Hard Landing check is done by the Flight Crew. MM 05-51-01 P201
(2) The flight crew must make a determination if a hard landing has occurred.
I would give you a picture of the chart but as a newby I'm not allowed to post attachments - sorry
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Ok.. so that means the Vertical G should just be at a value of 1.5 for maintenance checks?
Is not it a bit on the lower side?
Does the certification standard allow it?
Is not it a bit on the lower side?
Does the certification standard allow it?
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It depends on the Roll Angle - at Zero degrees role the Incremental load factor is 1.2. As you increase the roll angle the factor reduces to 0.6 at 6 degrees. Over 6 degrees the Load factor becomes irrelevant as a Part B inspection is mandatory.
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Thank you every one..
Consider me as a newb for a while with this.
In simple terms, if the load factor (vertical G) is 1.2 G or so with zero roll angle. Does that suffice for the hard landing checks?
Or that would be at 2.2 G value?
Consider me as a newb for a while with this.
In simple terms, if the load factor (vertical G) is 1.2 G or so with zero roll angle. Does that suffice for the hard landing checks?
Or that would be at 2.2 G value?
Not if the G required for the checks is 1.5 (2.5).
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So at zero roll the threshold for a part B inspection is 2.2G declining to 1.6G at 6 degrees roll - anything over 6 degrees roll requires Part B inspection irrespective.
Hope thats clear